US5297874A - Elastomeric bearing - Google Patents
Elastomeric bearing Download PDFInfo
- Publication number
- US5297874A US5297874A US07/971,228 US97122892A US5297874A US 5297874 A US5297874 A US 5297874A US 97122892 A US97122892 A US 97122892A US 5297874 A US5297874 A US 5297874A
- Authority
- US
- United States
- Prior art keywords
- interleaves
- reinforcing
- elastomeric
- thickness
- confronting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 52
- 239000013536 elastomeric material Substances 0.000 claims abstract description 40
- 239000000463 material Substances 0.000 claims description 10
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 230000006835 compression Effects 0.000 claims 1
- 238000007906 compression Methods 0.000 claims 1
- 239000010410 layer Substances 0.000 description 30
- 239000002184 metal Substances 0.000 description 12
- 238000010276 construction Methods 0.000 description 4
- 230000015556 catabolic process Effects 0.000 description 2
- 238000006731 degradation reaction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 229920000271 Kevlar® Polymers 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000003129 oil well Substances 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/40—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers
- F16F1/403—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers characterised by the shape of the non-elastic interengaging parts between the elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/42—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing
- F16F1/52—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses
- F16F1/54—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses loaded in compression and shear
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2236/00—Mode of stressing of basic spring or damper elements or devices incorporating such elements
- F16F2236/12—Mode of stressing of basic spring or damper elements or devices incorporating such elements loaded in combined stresses
- F16F2236/123—Mode of stressing of basic spring or damper elements or devices incorporating such elements loaded in combined stresses loaded in compression and shear
Definitions
- This invention relates to an elastomeric bearing and in particular, although not exclusively, to a heavy duty part-spherical type bearing for accommodating relative conical movement between two components.
- annular element of elastomeric material is provided between confronting annular faces of a pair of rigid members; typically those faces are inclined to both the longitudinal axis of the bearing and a plane perpendicular thereto and commonly are of a part-spherical shape.
- reinforcing metal interleaves may be provided in the elastomeric material, typically to lie in planes substantially parallel with the aforementioned inclined faces of the rigid members. Said reinforcing interleaves serve to transmit forces between successive elastomeric layers and do not directly transmit forces to or from structure external of the bearing.
- the metal interleaves prevent over-stressing of the elastomeric material interleaves interposed therebetween but themselves become subject to high stress by virtue of variations of the hydrostatic pressure in the elastomeric layers between which a metal interleaf is interposed.
- the bearing is required to accommodate a large degree of conical movement and/or is subject to a large number of cycles of conical movement there is a risk of failure of the metal interleaf.
- the present invention seeks to provide an elastomeric bearing of a kind comprising non-planar reinforcing interleaf layers in which the problem of over-stressing of the interleaf layers is mitigated or overcome.
- the present invention provides an elastomeric bearing comprising a pair of rigid members defining a pair of confronting and spaced apart bearing surfaces between which there is provided a non-planar element of elastomeric material, the elastomeric material having embedded therein a plurality of reinforcing interleaves of substantially rigid material each arranged to lie in a respective plane which is generally parallel in cross-section with said confronting surfaces and arranged to be acted upon substantially only by forces from said elastomeric material, wherein one or more of the reinforcing interleaves lying substantially mid-way between the confronting surfaces of the rigid members has a greater thickness than one or more of the reinforcing interleaves which lies closest to at least one of said confronting surfaces.
- the invention provides an elastomeric bearing in which only two reinforcing interleaves are provided, with that closest to one of said confronting surfaces being of smaller thickness than the other, it is envisaged that typically the elastomeric bearing shall comprise at least seven and more typically at least twelve reinforcing interleaves.
- the thickness of the reinforcing interleaves may vary progressively, increasing gradually from that interleaf nearest to a confronting surface to a maximum thickness for that interleaf which lies at or substantially at a position mid-way between the confronting surfaces.
- a or a group of reinforcing interleaves nearest one of said confronting surfaces may be of a first thickness and a or a second group at or substantially at a position mid-way between the confronting surfaces may be of a second thickness which is greater than said first thickness.
- the interleaves may vary in thickness in an asymmetric manner.
- the thickest layer may lie offset from a position at or substantially at the mid-way position.
- a layer nearest one confronting surface may be thicker than that nearest the other confronting surface.
- the invention particularly envisages that three groups of reinforcing interleaves will be provided, two groups being provided one each in the vicinity of a respective confronting surface and all of a common smaller thickness in comparison with a third group of two or more interleaves provided between said first groups and of a second, greater thickness than the interleaves of the first groups.
- one of said two groups may comprise layers thinner than the other of said two groups and thinner than the third group.
- the interleaves may be spaced by layers of elastomeric material each of a uniform thickness or said layers also may vary in thickness.
- Each confronting surface may comprise, for example, a pair of flat faces angled relative to one another thereby to provide a V-shape in cross-section, there being provided between said confronting surfaces a plurality of layers of elastomeric material and interposed reinforcing interleaves also of a V-shape in cross-section.
- the invention is, however, particularly applicable to elastomeric bearings of a kind in which said confronting surfaces are of an annular form, which may be cylindrical, frusto-conical or part-spherical shape.
- Each reinforcing interleaf may be of uniform thickness over its entire area or its thickness may be selectively varied, it being preferred in that case that the thickness is greater at regions of the layer at its periphery than regions lying centrally.
- Suitable materials for the reinforcing interleaves include substantially rigid materials such as steel, and for example layers of aromatic polyamide such as Kevlar, of carbon fibre reinforced plastics or other composites and thermoplastics.
- the elastomeric material forming the interlayers may be arranged to extend over the otherwise exposed edges of the reinforcing interleaves; alternatively those exposed edges may be covered by a sealing layer of another, typically elastomeric, material.
- the reinforcing interleaves will be free from any direct contact with structure external of the bearing unit.
- FIG. 1 is a longitudinal section through a part-spherical elastomeric bearing of the present invention.
- FIG. 2 is an enlarged view of the encircled part of FIG. 1, and
- FIGS. 3, 4 and 5 each show part longitudinal sections through part spherical elastomeric bearings in accordance with other embodiments of the present invention.
- FIG. 1 shows in longitudinal cross-section a heavy duty elastomeric bearing unit for use in accommodating relative conical movement between a sea bed structure (not shown) and a tether tube (not shown) which extends to a floating platform structure movable relative to the sea bed location of the bearing unit.
- the tethering arrangement of such a platform typically results in the elastomeric bearing unit being exposed to relative conical movement.
- the elastomeric bearing unit 10 comprises annular inner and outer rigid end members 11,12 which define confronting bearing surfaces 13,14 each of a part-spherical shape.
- the surface 14 of the outer rigid member 12 is of a concave form and that 13 of the inner rigid member is of a convex shape, each of the surfaces 13,14 having a common centre of curvature which is coincident with the longitudinal axis 21 of the bearing unit.
- a reinforced elastomeric assembly comprising layers 15 of elastomeric material which are in turn interposed between and bonded to metal reinforcing interleaves 16.
- eighteen metal interleaves are provided and arranged in three groups 17,18. Two of the groups each comprise four reinforcing interleaves 16a each of a thickness 5.8 mm while a third group comprises ten reinforcing interleaves 16b each of a thickness of 9.2 mm.
- the thicker layers 16b are arranged in a group 17 which lies interposed between the other two groups 18 which are thus substantially adjacent respective confronting surfaces 13,14.
- Each reinforcing interleaf 16a,16b is of a uniform thickness over its entire area.
- each interposed layer 15 of elastomeric material is of a uniform thickness and each of the layers 15 is of the same thickness.
- the elastomeric material of the layers 15 extends around the inner and outer peripheries of the metal reinforcing interleaves 16 to provide protective layers 19,20 to protect the exposed edges of the reinforcing interleaves and the bonded interfaces from degradation by fluid passing through the opening 22 defined by the annular bearing or fluid surrounding the outer surface of the bearing.
- Each reinforcing interleaf 16 is acted upon only by forces arising from or transmitted by said elastomeric material.
- the inner and outer rigid members 11,12 are provided with tapped bores 23 to facilitate location of the bearing unit relative to a sea bed structure and tether tube.
- FIG. 3 shows an elastomeric bearing similar to that of FIGS. 1 and 2 but with a different arrangement of metal interleaves 30-32.
- a central interleaf 30 is the thickest.
- the end interleaves 31 nearest the rigid end members 11,12 are thinnest and the other two layers 32 lying immediately either side of the central layer 30 are of an intermediate thickness.
- the thickness of the interleaves 30,31,32 varies progressively and in this embodiment is greatest at a position mid-way between the confronting surfaces 13,14.
- FIG. 4 shows a variation of the embodiment of FIG. 3 and in which each of the interleaves 35,36 and 37 is of a kind which varies in thickness over its area, each being thicker at inner and outer peripheral regions 38,39 than at a central region 34.
- the layers 35,36 and 37 otherwise correspond substantially with the layers 30,31 and 32 respectively of FIG. 3 in features such as spacing.
- FIG. 5 Another interleaved configuration is shown in FIG. 5. This is of an asymmetric type in which the central and thickest metal interleaf 40 lies displaced from a position mid-way between the confronting surfaces 13,14 and is nearest the surface 14. It is also asymmetric because the two interleaves 41 nearest the surface 14 are thinner than the two interleaves nearest the surface 13.
- FIGS. 3 to 5 for convenience and clarity only five interleaf layers have been shown.
- the invention envisages that a greater number of layers may be provided.
- two or more instead of one may be of a greatest thickness and layers of more than three different thicknesses may be utilized.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- Health & Medical Sciences (AREA)
- Child & Adolescent Psychology (AREA)
- Support Of The Bearing (AREA)
Abstract
Description
Claims (21)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/971,228 US5297874A (en) | 1990-01-06 | 1992-11-04 | Elastomeric bearing |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9012278 | 1990-01-06 | ||
GB909012278A GB9012278D0 (en) | 1990-06-01 | 1990-06-01 | Elastomeric bearing |
US70439991A | 1991-05-23 | 1991-05-23 | |
US07/971,228 US5297874A (en) | 1990-01-06 | 1992-11-04 | Elastomeric bearing |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US70439991A Continuation-In-Part | 1990-01-06 | 1991-05-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
US5297874A true US5297874A (en) | 1994-03-29 |
Family
ID=26297140
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US07/971,228 Expired - Fee Related US5297874A (en) | 1990-01-06 | 1992-11-04 | Elastomeric bearing |
Country Status (1)
Country | Link |
---|---|
US (1) | US5297874A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5609331A (en) * | 1995-09-05 | 1997-03-11 | Ford Motor Company | Torsion spring adjustment apparatus |
US5685527A (en) * | 1995-06-05 | 1997-11-11 | Ford Global Technologies, Inc. | Torsion spring adjustment apparatus |
WO2002042600A1 (en) * | 2000-11-21 | 2002-05-30 | Weatherford/Lamb, Inc. | Power tong frames |
US20040195988A1 (en) * | 2001-06-13 | 2004-10-07 | Buckingham Robert Oliver | Link assembly for a snake like robot arm |
US6803095B1 (en) | 2000-09-28 | 2004-10-12 | Lord Corporation | Composite shims having a laminate structure |
US20060027957A1 (en) * | 2004-08-04 | 2006-02-09 | Mueller Thomas G | Elastomeric bearing with modified cylindrical core |
US7188548B2 (en) | 2003-09-19 | 2007-03-13 | Weatherford/Lamb, Inc. | Adapter frame for a power frame |
US20090095112A1 (en) * | 2001-06-13 | 2009-04-16 | Robert Oliver Buckingham | Link Assembly With Defined Boundaries For A Snake Like Robot Arm |
US20090222133A1 (en) * | 2001-06-13 | 2009-09-03 | Robert Oliver Buckingham | System and Method for Controlling a Robotic Arm |
US20120314982A1 (en) * | 2008-04-26 | 2012-12-13 | Robert Cunningham | Spherical elastomeric bearing with improved shim thickness |
CN102829079A (en) * | 2012-08-28 | 2012-12-19 | 中国航空工业集团公司北京航空材料研究院 | Rigidity matching rubber supporting bearing |
CN105757118A (en) * | 2015-12-08 | 2016-07-13 | 中国航空工业集团公司北京航空材料研究院 | Radial-load-resistant long-service-life rubber supporting bearing |
US20180016002A1 (en) * | 2015-02-05 | 2018-01-18 | Sikorsky Aircraft Corporation | Abrasion resistant pivot bearing |
US10173770B2 (en) | 2014-09-22 | 2019-01-08 | Sikorsky Aircraft Corporation | Cylindrical elastomeric bearing with tapered shims |
FR3069592A1 (en) * | 2017-07-31 | 2019-02-01 | Aktiebolaget Skf | ELASTOMER BEARING COMPONENT WITH CORNER SHAFT |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB804438A (en) * | 1955-07-20 | 1958-11-12 | Metalastik Ltd | Improvements in or relating to rubber or the like spring supports |
US3228673A (en) * | 1963-08-26 | 1966-01-11 | William L Hinks | Laterally supported static load bearing |
GB1095598A (en) * | 1964-12-01 | 1967-12-20 | William Lloyd Hinks | A Laminated Support Fixture for Carrying a Load Subject to Dynamic Movement. |
US3504902A (en) * | 1967-08-22 | 1970-04-07 | Trw Inc | Pin stabilized laminated bearing flexible joint |
US4105266A (en) * | 1975-11-17 | 1978-08-08 | Lord Corporation | Laminated bearing with plural modulus layer |
US4123815A (en) * | 1975-05-02 | 1978-11-07 | Felt Products Mfg. Co. | Fixed point elastomeric bridge bearing and bridge assembly |
US4435097A (en) * | 1977-06-15 | 1984-03-06 | Barry Wright Corporation | Laminated bearing structures |
US4518368A (en) * | 1983-06-08 | 1985-05-21 | Barry Wright Corporation | Coupling |
US4734081A (en) * | 1985-11-04 | 1988-03-29 | Bell Helicopter Textron Inc. | Constant velocity elastomeric bearing joint |
US4765758A (en) * | 1985-01-07 | 1988-08-23 | Barry Wright Corporation | Laminated bearing |
-
1992
- 1992-11-04 US US07/971,228 patent/US5297874A/en not_active Expired - Fee Related
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB804438A (en) * | 1955-07-20 | 1958-11-12 | Metalastik Ltd | Improvements in or relating to rubber or the like spring supports |
US3228673A (en) * | 1963-08-26 | 1966-01-11 | William L Hinks | Laterally supported static load bearing |
GB1095598A (en) * | 1964-12-01 | 1967-12-20 | William Lloyd Hinks | A Laminated Support Fixture for Carrying a Load Subject to Dynamic Movement. |
US3504902A (en) * | 1967-08-22 | 1970-04-07 | Trw Inc | Pin stabilized laminated bearing flexible joint |
US4123815A (en) * | 1975-05-02 | 1978-11-07 | Felt Products Mfg. Co. | Fixed point elastomeric bridge bearing and bridge assembly |
US4105266A (en) * | 1975-11-17 | 1978-08-08 | Lord Corporation | Laminated bearing with plural modulus layer |
US4435097A (en) * | 1977-06-15 | 1984-03-06 | Barry Wright Corporation | Laminated bearing structures |
US4518368A (en) * | 1983-06-08 | 1985-05-21 | Barry Wright Corporation | Coupling |
US4765758A (en) * | 1985-01-07 | 1988-08-23 | Barry Wright Corporation | Laminated bearing |
US4734081A (en) * | 1985-11-04 | 1988-03-29 | Bell Helicopter Textron Inc. | Constant velocity elastomeric bearing joint |
Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5685527A (en) * | 1995-06-05 | 1997-11-11 | Ford Global Technologies, Inc. | Torsion spring adjustment apparatus |
US5609331A (en) * | 1995-09-05 | 1997-03-11 | Ford Motor Company | Torsion spring adjustment apparatus |
US6803095B1 (en) | 2000-09-28 | 2004-10-12 | Lord Corporation | Composite shims having a laminate structure |
US20040035573A1 (en) * | 2000-11-21 | 2004-02-26 | Bernd-Georg Pietras | Power tong frames |
WO2002042600A1 (en) * | 2000-11-21 | 2002-05-30 | Weatherford/Lamb, Inc. | Power tong frames |
US7921750B2 (en) | 2000-11-21 | 2011-04-12 | Weatherford/Lamb, Inc. | Power tong frames |
US20040195988A1 (en) * | 2001-06-13 | 2004-10-07 | Buckingham Robert Oliver | Link assembly for a snake like robot arm |
US8205522B2 (en) | 2001-06-13 | 2012-06-26 | Oliver Crispin Robotics Limited | Link assembly with defined boundaries for a snake like robot arm |
US8219246B2 (en) | 2001-06-13 | 2012-07-10 | Oliver Crispin Robotics Limited | System and method for controlling a robotic arm |
US20090095112A1 (en) * | 2001-06-13 | 2009-04-16 | Robert Oliver Buckingham | Link Assembly With Defined Boundaries For A Snake Like Robot Arm |
US7543518B2 (en) * | 2001-06-13 | 2009-06-09 | Oliver Crispin Robotics Limited | Link assembly for a snake like robot arm |
US20090222133A1 (en) * | 2001-06-13 | 2009-09-03 | Robert Oliver Buckingham | System and Method for Controlling a Robotic Arm |
US7188548B2 (en) | 2003-09-19 | 2007-03-13 | Weatherford/Lamb, Inc. | Adapter frame for a power frame |
US20060027957A1 (en) * | 2004-08-04 | 2006-02-09 | Mueller Thomas G | Elastomeric bearing with modified cylindrical core |
US7097169B2 (en) | 2004-08-04 | 2006-08-29 | Skf Usa Inc. | Elastomeric bearing with modified cylindrical core |
US20120314982A1 (en) * | 2008-04-26 | 2012-12-13 | Robert Cunningham | Spherical elastomeric bearing with improved shim thickness |
US8911153B2 (en) * | 2008-04-26 | 2014-12-16 | Sikorsky Aircraft Corporation | Spherical elastomeric bearing with improved shim thickness |
EP2112064A3 (en) * | 2008-04-26 | 2015-10-28 | Sikorsky Aircraft Corporation | Spherical elastomeric bearing with improved shim thickness |
CN102829079A (en) * | 2012-08-28 | 2012-12-19 | 中国航空工业集团公司北京航空材料研究院 | Rigidity matching rubber supporting bearing |
CN102829079B (en) * | 2012-08-28 | 2015-07-15 | 中国航空工业集团公司北京航空材料研究院 | Rigidity matching rubber supporting bearing |
US10173770B2 (en) | 2014-09-22 | 2019-01-08 | Sikorsky Aircraft Corporation | Cylindrical elastomeric bearing with tapered shims |
US20180016002A1 (en) * | 2015-02-05 | 2018-01-18 | Sikorsky Aircraft Corporation | Abrasion resistant pivot bearing |
US10272996B2 (en) * | 2015-02-05 | 2019-04-30 | Sikorsky Aircraft Corporation | Abrasion resistant pivot bearing |
CN105757118A (en) * | 2015-12-08 | 2016-07-13 | 中国航空工业集团公司北京航空材料研究院 | Radial-load-resistant long-service-life rubber supporting bearing |
FR3069592A1 (en) * | 2017-07-31 | 2019-02-01 | Aktiebolaget Skf | ELASTOMER BEARING COMPONENT WITH CORNER SHAFT |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5297874A (en) | Elastomeric bearing | |
US4958812A (en) | Suspension spring system | |
US4968010A (en) | Slotted disc and elastomeric matrix damper assembly | |
US3504902A (en) | Pin stabilized laminated bearing flexible joint | |
JP5373274B2 (en) | Anti-vibration structure | |
JPS5855377B2 (en) | multilayer support | |
US4570979A (en) | Flexible joint means | |
US4765758A (en) | Laminated bearing | |
US4006892A (en) | Compression mounting | |
US3228673A (en) | Laterally supported static load bearing | |
EP0946833A1 (en) | Reinforced elastomeric spring | |
GB1591483A (en) | Joint assembly | |
US3504904A (en) | Retainer ring button laminated bearing flexible joint | |
US4105264A (en) | Processing roller having reinforcing jacket of hard metal | |
SE500084C2 (en) | Resilient, power transferring spring element | |
GB1583823A (en) | Hydraulic transmission drive assembly | |
US6371461B1 (en) | Elastic bush with two armatures; torque take up connecting rod equipped with a bush of this kind | |
US4846509A (en) | Flexible joint means | |
GB2244540A (en) | Elastomeric bearing | |
CA2241250C (en) | Ribbed diaphragm | |
US4881921A (en) | Flexible shaft coupling with coated grid | |
US4838736A (en) | Resilient bush | |
JPH041206B2 (en) | ||
GB2121905A (en) | Flexible joint | |
GB2159224A (en) | Flexible joint |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: DUNLOP LIMITED, UNITED KINGDOM Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:RAINES, KENNETH W. J.;REEL/FRAME:006316/0310 Effective date: 19920929 |
|
FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
|
FPAY | Fee payment |
Year of fee payment: 4 |
|
AS | Assignment |
Owner name: BTR INDUSTRIES LIMITED, ENGLAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:DUNLOP LIMITED;REEL/FRAME:009328/0963 Effective date: 19980522 |
|
REMI | Maintenance fee reminder mailed | ||
LAPS | Lapse for failure to pay maintenance fees | ||
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
|
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20020329 |